发明名称 RADIAL TIRE FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a radial tire for an aircraft having excellent abrasion resistant characteristic and excellent belt durability. SOLUTION: A peripheral side of a crown part 3 of a radial carcass 2 is provided with an endless belt 4, an end belt 7 and a tread part 8 in order. A protecting layer 9 is embedded in the tread part 8, and a plurality of circumferential grooves 10 are arranged in the tread surface of the tread part 8, and a low-heat-generation type space rubber 13 is arranged in the inside part of the tread part 8 extended from an end surface 11 of the endless belt 4 to an end surface 12 of the protecting layer 9. The most outside circumferential groove 10a is arranged at the predetermined position, and a curvature radius R of the crown part of the tread part 8 pinched between both the most outside peripheral grooves 10a is set at a value in a range 1.0-2.0 times of the tread width TW. An interlayer rubber 14 having a thickness of 0.5-1.0 mm and a breakdown elongation of 330-400% is arranged between the space rubber 13 and the end surface 11 of the endless belt 4. COPYRIGHT: (C)2003,JPO
申请公布号 JP2003226110(A) 申请公布日期 2003.08.12
申请号 JP20020026726 申请日期 2002.02.04
申请人 BRIDGESTONE CORP 发明人 ITAMI DAISUKE
分类号 B60C9/18;B60C11/00;B60C11/04;(IPC1-7):B60C9/18 主分类号 B60C9/18
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